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WORTMANN FX 69-274 (fx69274-il)

WORTMANN FX 69-274 - Wortmann FX 69-274 airfoil


Airfoil fx69274-il
Details Dat file Parser  
(fx69274-il) WORTMANN FX 69-274
Wortmann FX 69-274 airfoil
Max thickness 27.4% at 33.9% chord.
Max camber 3.2% at 37.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
WORTMANN FX 69-274
1.00000     0.00000
0.99893     0.00743
0.99572     0.00808
0.99039     0.00929
0.98296     0.01107
0.97347     0.01343
0.96194     0.01638
0.94844     0.02000
0.93301     0.02441
0.91573     0.02957
0.89668     0.03550
0.87592     0.04214
0.85355     0.04943
0.82967     0.05743
0.80438     0.06600
0.77779     0.07500
0.75000     0.08429
0.72114     0.09371
0.69134     0.10329
0.66072     0.11271
0.62941     0.12186
0.59755     0.13057
0.56526     0.13886
0.53270     0.14629
0.50000     0.15300
0.46730     0.15857
0.43474     0.16314
0.40245     0.16643
0.37059     0.16829
0.33928     0.16871
0.30866     0.16786
0.27886     0.16529
0.25000     0.16143
0.22221     0.15614
0.19562     0.14943
0.17033     0.14157
0.14645     0.13271
0.12408     0.12286
0.10332     0.11229
0.08427     0.10129
0.06699     0.08971
0.05156     0.07800
0.03806     0.06614
0.02653     0.05443
0.01704     0.04286
0.00961     0.03157
0.00428     0.02071
0.00107     0.01043
0.00000     0.00000
0.00107     -0.00942
0.00428     -0.01843
0.00961     -0.02714
0.01704     -0.03543
0.02653     -0.04357
0.03806     -0.05114
0.05156     -0.05857
0.06699     -0.06557
0.08427     -0.07214
0.10332     -0.07829
0.12408     -0.08386
0.14645     -0.08900
0.17033     -0.09357
0.19562     -0.09742
0.22221     -0.10057
0.25000     -0.10300
0.27886     -0.10457
0.30866     -0.10543
0.33928     -0.10543
0.37059     -0.10457
0.40245     -0.10300
0.43474     -0.10071
0.46730     -0.09786
0.50000     -0.09429
0.53270     -0.09000
0.56526     -0.08543
0.59755     -0.08029
0.62941     -0.07486
0.66072     -0.06914
0.69134     -0.06329
0.72114     -0.05729
0.75000     -0.05129
0.77779     -0.04543
0.80438     -0.03971
0.82967     -0.03429
0.85355     -0.02943
0.87592     -0.02486
0.89668     -0.02070
0.91573     -0.01757
0.93301     -0.01475
0.94844     -0.01243
0.96194     -0.01056
0.97347     -0.00914
0.98296     -0.00819
0.99039     -0.00757
0.99572     -0.00711
0.99893     -0.00686
1.00000     0.00000
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Polars for WORTMANN FX 69-274 (fx69274-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx69274-il50,00091.6 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   fx69274-il100,00091.7 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx69274-il200,000936 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx69274-il500,000965.4 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx69274-il1,000,000981.3 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
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